CN117716214A - Method of operating a coriolis mass flowmeter - Google Patents
Method of operating a coriolis mass flowmeter Download PDFInfo
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- CN117716214A CN117716214A CN202280050679.8A CN202280050679A CN117716214A CN 117716214 A CN117716214 A CN 117716214A CN 202280050679 A CN202280050679 A CN 202280050679A CN 117716214 A CN117716214 A CN 117716214A
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- 238000000034 method Methods 0.000 title claims abstract description 45
- 238000005259 measurement Methods 0.000 claims abstract description 115
- 238000005452 bending Methods 0.000 claims abstract description 28
- 230000000694 effects Effects 0.000 claims description 15
- 238000012937 correction Methods 0.000 claims description 12
- 230000008859 change Effects 0.000 claims description 5
- 238000012544 monitoring process Methods 0.000 claims description 4
- 244000309466 calf Species 0.000 description 10
- 230000008878 coupling Effects 0.000 description 7
- 238000010168 coupling process Methods 0.000 description 7
- 238000005859 coupling reaction Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000009529 body temperature measurement Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- 230000004044 response Effects 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 230000005520 electrodynamics Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000012886 linear function Methods 0.000 description 2
- 230000010355 oscillation Effects 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 230000011664 signaling Effects 0.000 description 2
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000009530 blood pressure measurement Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 238000013213 extrapolation Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000246 remedial effect Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/76—Devices for measuring mass flow of a fluid or a fluent solid material
- G01F1/78—Direct mass flowmeters
- G01F1/80—Direct mass flowmeters operating by measuring pressure, force, momentum, or frequency of a fluid flow to which a rotational movement has been imparted
- G01F1/84—Coriolis or gyroscopic mass flowmeters
- G01F1/8409—Coriolis or gyroscopic mass flowmeters constructional details
- G01F1/8436—Coriolis or gyroscopic mass flowmeters constructional details signal processing
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- Engineering & Computer Science (AREA)
- Signal Processing (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Volume Flow (AREA)
Abstract
The invention relates to a method (100) for operating a coriolis mass flowmeter having at least one vibrating measuring tube for a conductive medium, comprising: exciting (110 a) a first symmetrical bending vibration mode of the at least one measurement tube; exciting (110 b) a second symmetrical bending vibration mode of the at least one measurement tube; determining (120 a) a first mass flow rate measurement based on a first coriolis deformation of the at least one measurement tube and a first stored mode-specific zero error value; determining (120 b) a second mass flow rate measurement based on a second coriolis deformation of the at least one measurement tube and a second stored mode-specific zero error value; and determining (130) a zero offset value for the mass flow rate measurement as a function of the offset between the first mass flow rate measurement and the second mass flow rate measurement.
Description
Technical Field
The invention relates to a method for operating a Coriolis mass flowmeter having at least one measuring tube for a conductive medium that can vibrate.
Background
During the operation of any measuring device, measurement errors can occur, including in the case of coriolis mass flowmeters, wherein in principle a distinction is made between zero point errors and span errors. The zero point error occurs in particular due to the asymmetry of the vibration behaviour of the measuring tube.
International publication WO 2019/045703 A1 describes that the stiffness of the measuring tube can change over time, for example, due to wear or corrosion, wherein zero point errors do not change. For example, measurement errors due to a changed measurement tube stiffness can be identified based on the ratio of excitation signals to sensor signals.
Disclosure of Invention
In contrast, the asymmetry of the changing zero point may be caused by uneven attenuation and cannot be detected by the operation method described so far. Of course, in the case of factory calibration, the corresponding zero point error can be determined for the vibration mode considered in the stationary medium (i.e. the flow rate is zero) and can be subtracted accordingly when calculating the flow measurement value. However, during ongoing measurement operations, it is not possible with previous monitoring methods to detect whether the zero point error has changed from the state at the time of factory calibration. This will therefore lead to measurement errors that are not detected during the measurement operation when determining the mass flow rate. It is therefore an object of the present invention to provide a remedial action and in particular to specify a method of operation that is capable of detecting a changing zero point in time. According to the invention, this object is achieved by a method according to independent claim 1.
The method according to the invention for operating a coriolis mass flowmeter having at least one vibrating measuring tube for a conductive medium comprises:
exciting a first symmetrical bending vibration mode of the at least one measurement tube;
exciting a second symmetrical bending vibration mode of the at least one measurement tube;
determining a first mass flow rate measurement based on the first stored mode-specific zero error value and a first coriolis deformation of the at least one measurement tube;
determining a second mass flow rate measurement based on a second stored mode-specific zero error value and a second coriolis deformation of the at least one measurement tube; and
a zero offset value of the mass flow rate measurement is determined as a function of the offset between the first mass flow rate measurement and the second mass flow rate measurement.
The first coriolis deformation is caused by inertial forces of the flow medium in response to vibrations of the measurement tube in a first symmetric flexural vibration mode. The second coriolis deformation is caused by inertial forces of the flow medium in response to vibrations of the measurement tube in a second symmetric flexural vibration mode.
Since zero point errors are not readily available during ongoing measurement operations, a deviation value between the first mass flow rate measurement and the second mass flow rate measurement is determined here and is interpreted as a zero point deviation value, i.e. as a deviation between the time variations of the zero point errors of the first mass flow rate measurement or the second mass flow rate measurement.
In one refinement of the invention, the method further comprises monitoring zero offset values and signaling an error condition if at least one of the zero offset values exceeds a threshold value.
In this case, the starting point of the invention is: a large zero offset value requires a sufficient variation in zero error of the mass flow rate measurement under consideration. In this respect, the method according to the invention indicates the zero offset value as an indication of zero error. However, if the zero point error development of the considered mass flow rate measurement is the same, the method according to the present invention will fail because a variable zero point deviation value will not be detected. However, this is a very theoretical problem, since a consistent development of zero point errors is very unlikely. As already mentioned at the outset, zero point errors are a result of asymmetries in the vibration behaviour of the measuring tube, which occur in particular due to local attenuation of the asymmetric distribution (for example, due to accumulation and/or micro wear). However, these local attenuations have different effects on the relevant vibration modes, since the distribution of the vibration energy affected by the local attenuations is very different along the measuring tube between the vibration modes considered.
In one refinement of the invention, determining the first mass flow rate measurement and the second mass flow rate measurement comprises in each case: determining preliminary mass flow rate measurements based in each case on corresponding coriolis deformations of at least one measuring tube; determining correction factors for the first preliminary mass flow rate measurement and the second preliminary mass flow rate measurement in each case for influencing the mass flowmeter by means of resonator effects due to the gas load of the medium conducted in the measuring tube; and correcting the two preliminary mass flow rate measurements with the corresponding mass flow rate correction factors.
In an improvement of the invention, the method further comprises: checking whether the mass flow meter is affected by a resonator effect due to a gas load of a medium conducted in the measurement pipe based on natural frequencies of the plurality of flexural vibration modes; wherein in this case the determination of the first mass flow rate measurement and the second mass flow rate measurement comprises in each case: determining preliminary mass flow rate measurements based in each case on corresponding coriolis deformations of at least one measuring tube; determining correction factors for the first preliminary mass flow rate measurement and the second preliminary mass flow rate measurement in each case for influencing the mass flowmeter by means of resonator effects due to the gas load of the medium conducted in the measuring tube; and correcting the two preliminary mass flow rate measurements with the corresponding mass flow rate correction factors.
In one refinement of the invention, the method is performed in a stationary medium, wherein the method further comprises:
updating the first zero error value based on the first mass flow rate measurement; and
a second zero error value is updated based on the second mass flow rate measurement.
In one refinement, the method further comprises: before determining the zero offset value, correcting the first and second mass flow rate measurements with respect to an effect of at least one of the following influencing variables: medium pressure, medium temperature and reynolds number. These corrections ensure that influencing variables that have different effects on different bending vibration modes do not lead to any falsification of the zero offset value.
The coriolis mass flowmeter according to the present invention includes: at least one measuring tube for conducting a medium; at least one exciter for exciting bending vibration modes of the at least one measuring tube; at least one sensor for detecting bending vibrations of the at least one measuring tube; measurement and operation circuitry configured to drive the actuator, detect a signal of the at least one sensor, determine a mass flow rate measurement based on the signal of the at least one sensor, and perform the method of any one of claims 1 to 7.
Drawings
The invention is explained in more detail on the basis of exemplary embodiments shown in the drawings. In the figure:
FIG. 1a shows a side view of an exemplary embodiment of a coriolis mass flowmeter according to the present invention for performing a method according to the present invention;
fig. 1b shows a spatial illustration of an exemplary embodiment of the coriolis mass flowmeter according to the invention from fig. 1 a.
FIG. 2a shows a schematic view of a bending line of a first symmetrical bending vibration mode;
FIG. 2b shows a schematic diagram of Coriolis deformation due to mass flow in a first symmetric bending vibration mode and measurement tube vibration;
FIG. 2c shows a schematic diagram of the effect of local attenuation on flow measurement based on a first symmetric bending vibration mode;
FIG. 3a shows a schematic view of a bending line of a second symmetrical bending vibration mode;
FIG. 3b shows a schematic diagram of Coriolis deformation due to measurement tube vibration and mass flow in a second symmetric bending vibration mode;
FIG. 3c shows a schematic diagram of the effect of local attenuation on flow measurement based on a second symmetric bending vibration mode;
fig. 4a shows a flow chart of an exemplary embodiment of a method for operating a coriolis mass flowmeter according to the present invention;
FIG. 4b shows a detailed flow chart of partial steps from the exemplary embodiment of the method according to the present invention of FIG. 4 a; and
fig. 4c shows a flow chart of an improved exemplary embodiment of a method for operating a coriolis mass flowmeter according to the present invention.
Detailed Description
Fig. 1a and 1b show an exemplary embodiment of a coriolis mass flowmeter 2 according to the invention, which is designed to carry out the method according to the invention. The coriolis mass flowmeter 2 has two vibrating-mounted measuring tubes a and B, each having an arcuate shape and extending parallel to each other. The coriolis mass flowmeter 2 can be inserted into a pipe (not shown) such that fluid flowing in the pipe flows through two measurement pipes A, B. At the inlet side and at the outlet side, the measuring tubes A, B are each enclosed in a flow diverter or collector 4, 6, which are rigidly connected to each other by a support tube T. The inlet-side end and the outlet-side end of the measuring tube are thus also coupled to the support tube T, whereby the relative movement between the inlet-side end and the outlet-side end of the measuring tube is effectively suppressed.
Between the two measuring tubes A, B, an electrical exciter 8 is arranged, by means of which electric exciter 8 the two measuring tubes A, B can be excited to perform bending oscillations relative to one another, wherein the free oscillation length of the measuring tube A, B is defined by the coupling elements 10, 11, the measuring tubes being mechanically coupled on the inlet side and on the outlet side by the coupling elements 10, 11. Between the two measuring pipes A, B, the electrodynamic vibration sensors 14,16 are arranged on the inlet side portion and the outlet side portion. The coriolis mass flowmeter 2 further comprises an arithmetic and evaluation circuit 18 for feeding the exciter 8 with an exciter current and for detecting and evaluating the measurement signals of the electrodynamic vibration transducers 14, 16. The coriolis mass flowmeter 2 further comprises a first temperature sensor (not shown here) which is arranged, for example, on the first coupling element 10 in order to determine a first temperature measurement value which represents the temperature of the measuring tube A, B. The positioning of the temperature sensor on the coupling element 10 is appropriate in respect of the coupling element being connected only to the measuring tube A, B, so that the temperature of the coupling element is largely defined by the temperature of the measuring tube. Also, the temperature sensor can be arranged on one of the measuring tubes, in particular outside the vibrating portion defined by the coupling element, whereby a shorter response time of the temperature sensor is achieved. The measurement and operating circuit 18 is configured to detect a measurement signal from a temperature sensor, which measurement signal represents a temperature measurement value, which temperature measurement value for example enters into the calculation of the temperature-dependent elastic modulus.
In order to carry out the method according to the invention, it is advantageous if the measuring and operating circuit also has an input for the pressure measurement value p, so that the medium pressure can be taken into account when carrying out the method according to the invention for operating a coriolis mass flowmeter.
While fig. 1a and 1b show an exemplary embodiment of a coriolis mass flowmeter having a pair of measurement tubes bent in a rest position, the present invention is equally applicable to coriolis mass flowmeters having a single measurement tube or having multiple pairs of measurement tubes. Similarly, instead of the shown measuring tube which is bent in mirror geometry with respect to the transverse plane of the measuring tube in the rest position, it is also possible to implement the invention using even S-shaped measuring tubes or straight measuring tubes.
The principle on which the invention is based is described below with reference to fig. 2a to c and fig. 3a to c. Mass flow measurement based on coriolis principleDeviations of the vibrations from their ideal symmetrical shape, which are caused by the superposition of anti-symmetrical coriolis deformations whose magnitude is proportional to the mass flow, are evaluated. Fig. 2a and 3a schematically show a bending line a of the first two symmetrical bending vibration modes of the measuring tube along the longitudinal coordinate ζ of the measuring tube 1 (ζ)、a 3 (ζ), wherein fig. 2b and 3b each represent an associated coriolis deformation c of the measuring tube 1 (ζ),c 3 (ζ) each attached to an associated bending vibration mode. In the present context, the detailed curve is not critical. It is only necessary that the coriolis deformations of the different modes have their maximum and minimum values at different positions in the longitudinal direction. The illustrated coriolis deformations thus have different cross sensitivities to the local attenuation, since the local attenuation at the maximum value of the coriolis deformations has a significantly different effect than the local attenuation at the zero point of the coriolis deformations. This local attenuation (e.g. as may occur due to accumulation formation and/or micro-wear or gaseous inclusions) acts as zero point error, as shown in fig. 2c and 3 c. Each curve shows a different local attenuated flow measurement Δo of the first and second symmetrical bending vibration modes as a function of the position ζ of the attenuation and the associated envelope curve H1, H3 1 (ζ),Δo 3 (ζ) experimentally determined variation. By applying a contact surface on the measuring tube of about 1cm 2 Is used to achieve damping. In normal measurement operations, these zero errors cannot be identified using methods according to the prior art. However, according to the present invention, by comparing two mass flow rate measurements based on different flexural vibration modes, it can be determined whether a deviation has occurred. This deviation can be designated as zero point error if other causes can be excluded.
The sequence of the method for zero point monitoring according to the invention will now be explained in more detail with reference to the exemplary embodiment shown in fig. 4 a. The method 100 according to the invention starts with exciting 110a first symmetrical bending vibration mode of at least one measuring tube and exciting 110b a second symmetrical bending vibration mode of at least one measuring tube. In particular two symmetrical bending vibration modes are excited simultaneously.
A first mass flow rate measurement is determined 120a based on a first coriolis deformation of the at least one measurement tube and a first stored mode-specific zero error value, and a second mass flow rate measurement is determined 120b based on a second coriolis deformation of the at least one measurement tube and a second stored mode-specific zero error value. Mode-specific time delay τ between maximum speeds of two vibration sensors i Is a linear function of (a) to determine each mass flow rate measurementAccording to the following:
wherein, calf i And o i The mode-specific calibration factor and the mode-specific zero-point error are each described, which are determined, for example, during an initial adjustment and are stored in a memory of the measuring and operating circuit.
In the ideal case of a combination of the above-mentioned,is applicable to mass flow rate measurements acquired simultaneously based on two different bending vibration modes, where ε is a threshold value for zero offset. To check the extent to which this condition is fulfilled, the difference between the two mass flow rate measurements is determined 130 +.>And designates the difference amount as a zero-point deviation value and then stores the zero-point deviation value.
The zero offset value is then compared 140 to a threshold epsilon, wherein an error is signaled 150 when the zero offset value exceeds the threshold. Otherwise, if there is no such signaling, then a new run of the method begins. The threshold value can be, for example, 0.1% of the measurement range.
In one refinement, the time development of the zero offset value can also be monitored and extrapolated as a linear function of time, for example, wherein, depending on the extrapolation, a need for maintenance can also be signaled if it is expected that the threshold value will be exceeded within a defined period of time (for example one month or one week).
Fig. 4b now shows in detail how the determination 120a, 120b of the mass flow rate measurement is made. In-mode specific calibration factor calf i With mode-specific cross sensitivity, the effect of the zero offset value must first be corrected before it can be determined. In a first substep, a mode-specific time delay τ is determined 121a, 121b simultaneously i . Subsequently, a preliminary calibration factor calf specific to the 121a, 121b mode is calculated according to the following equation i ：
calf＇ i ＝calf ref i Π j K i，j ，
Wherein, calf ref i Describes a mode-specific calibration factor under reference conditions, and K i,j Is a mode-specific correction factor that corrects for one of the effects of density, viscosity, temperature, pressure and medium compressibility in each case.
Details for correcting the influence of density, viscosity, temperature and pressure are familiar to the person skilled in the art of flow measurement and are described, for example, in EP 0261 435 B1, DE 102007 061 585 A1, DE 102007008 197 A1 and DE 102009012474 A1 and the prior art cited therein.
Details for correcting the influence of the compressibility of the medium are described, for example, in EP 3394575 B1.
Based on a preliminary mode specific calibration factor calf' i Calculating 122a, 122b preliminary mode specific mass flow rate measurements
Mass flow rate measurement specified by preliminary modeThe 123a, 123b is then determined to be the most optimal according toFinal mode specific calibration factor:
calf i ＝calf＇ i K j Rc ，
wherein K is j Re Is a factor for mode-specific reynolds number correction.
Details concerning the reynolds number correction are described, for example, in EP 1 055 102 B1.
Using the final mode-specific calibration factor calf determined in this way i Finally, mode-specific mass flow rate measurements are calculated 124a, 124b according to the following equation:
thereby completing method steps 120a, 120b.
Fig. 4c finally shows a modified embodiment 100' of the method, which allows updating the mode-specific zero error o i It is assumed that information is available as to whether the traffic is actually zero. For example, if the status "off" causes an interruption of the flow to be monitored, this can be ensured by the status information of the valve. An inquiry 125 as to whether the valve is open is provided after the calculation 120a, 120b of the mass flow rate measurement. In the affirmative case, the method continues to determine 130 the amount of difference between the mass flow rate measurements as before. In the negative case, however, it is then checked 126 whether the mass flow rate measurement deviates from zero by no more than a tolerance value. In the affirmative, the method starts over again from scratch. In the negative case, however, the check is followed by an analysis 127 of the mode-specific zero point error o i Which corresponds to a mass flow rate measurement, since the latter must currently be zero. For example, it is checked whether a mode-specific alarm limit value for the zero point error is exceeded, wherein an error message is output in this case.
Likewise, it is also determined, for example, at what average rate of change the zero point error has changed since the last safety determination. According to one embodiment of the invention, it is thus possible to target when similar variations and/or zero-crossing errors can be expected under the same process conditionsThe mode-specific alarm limit value of the difference is used to make the prediction. A message is output regarding the expected point in time. Finally, the current mode-specific mass flow rate measurement is taken before a new run of the method beginsStore 128 is a new mode specific zero point error o i 。/>
Claims (8)
1. A method (100) for operating a coriolis mass flowmeter having at least one vibratable measurement tube for a conductive medium, the method comprising:
exciting (110 a) a first symmetrical bending vibration mode of the at least one measurement tube;
exciting (110 b) a second symmetrical bending vibration mode of the at least one measurement tube;
determining (120 a) a first mass flow rate measurement based on a first coriolis deformation of the at least one measurement tube and a first stored mode-specific zero error value;
determining (120 b) a second mass flow rate measurement based on a second coriolis deformation of the at least one measurement tube and a second stored mode-specific zero error value; and
a zero offset value of a mass flow rate measurement as a function of an offset between the first mass flow rate measurement and the second mass flow rate measurement is determined (130).
2. The method (100) of claim 1, further comprising:
-monitoring (140) the zero offset value; and
if at least one zero-offset value exceeds a threshold value, an error condition is signaled (150).
3. The method of claim 1, further comprising:
a rate of change of the zero offset value is determined (150), and an error state is signaled if the rate of change of the zero offset value exceeds a threshold.
4. The method of any of the preceding claims, wherein determining the first and second mass flow rate measurements comprises in each case:
determining preliminary mass flow rate measurements in each case based on corresponding coriolis deformations of the at least one measurement tube;
determining correction factors for a first preliminary mass flow rate measurement and a second preliminary mass flow rate measurement in each case for influencing the mass flowmeter by a resonator effect due to a gas load of the medium conducted in the measuring tube; and
the two preliminary mass flow rate measurements are corrected with corresponding mass flow rate correction factors.
5. The method of claim 1, further comprising:
checking whether the mass flow meter is affected by a resonator effect due to a gas load of the medium conducted in the measurement pipe based on natural frequencies of a plurality of flexural vibration modes;
wherein in this case the determination of the first and second mass flow rate measurements comprises in each case:
determining preliminary mass flow rate measurements in each case based on the corresponding coriolis deformation mode of the at least one measurement tube;
determining correction factors for the first preliminary mass flow rate measurement and the second preliminary mass flow rate measurement in each case for influencing the mass flow meter by resonator effects due to the gas load of the medium conducted in the measuring tube; and
the two preliminary mass flow rate measurements are corrected with corresponding mass flow rate correction factors.
6. The method according to one of the preceding claims,
wherein the method is performed in a stationary medium, the method further comprising:
updating the first zero error value based on the first mass flow rate measurement; and
the second zero error value is updated based on the second mass flow rate measurement.
7. The method of one of the preceding claims, further comprising:
correcting the first and second mass flow rate measurements with respect to the effect of at least one of the following influencing variables prior to determining the zero offset value: medium pressure, medium temperature and reynolds number.
8. A coriolis mass flowmeter (2) comprising:
-at least one measuring tube (a, B), said at least one measuring tube (a, B) being for conducting a medium;
-at least one exciter (8), the at least one exciter (8) being arranged to excite bending vibration modes of the at least one measuring tube (a, B);
at least one sensor (14, 16), the at least one sensor (14, 16) being adapted to detect bending vibrations of the at least one measuring tube;
-a measurement and operation circuit (18), the measurement and operation circuit (18) being configured to drive the exciter (8), to detect signals from the at least one sensor (14, 16), to determine a mass flow rate measurement based on the signals from the at least one sensor (14, 16), and to perform the method according to any one of claims 1 to 7.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102021118961.6A DE102021118961A1 (en) | 2021-07-22 | 2021-07-22 | Method of operating a Coriolis mass flow meter |
| DE102021118961.6 | 2021-07-22 | ||
| PCT/EP2022/068450 WO2023001534A1 (en) | 2021-07-22 | 2022-07-04 | Method for operating a coriolis mass flowmeter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117716214A true CN117716214A (en) | 2024-03-15 |
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ID=82458653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202280050679.8A Pending CN117716214A (en) | 2021-07-22 | 2022-07-04 | Method of operating a coriolis mass flowmeter |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP4374144A1 (en) |
| CN (1) | CN117716214A (en) |
| DE (1) | DE102021118961A1 (en) |
| WO (1) | WO2023001534A1 (en) |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3505166A1 (en) * | 1985-02-15 | 1986-08-21 | Danfoss A/S, Nordborg | MASS FLOW MEASURING DEVICE ACCORDING TO THE CORIOLIS PRINCIPLE |
| US4823614A (en) * | 1986-04-28 | 1989-04-25 | Dahlin Erik B | Coriolis-type mass flowmeter |
| DE3632800A1 (en) | 1986-09-26 | 1988-04-07 | Flowtec Ag | MASS FLOW MEASURING DEVICE WORKING ACCORDING TO THE CORIOLIS PRINCIPLE |
| ATE235672T1 (en) | 1998-12-11 | 2003-04-15 | Flowtec Ag | CORIOLIS MASS FLOW/DENSITY METER |
| JP4761134B2 (en) | 2006-02-17 | 2011-08-31 | 独立行政法人産業技術総合研究所 | Mass flow meter |
| DE102007061585A1 (en) | 2006-12-18 | 2008-06-19 | Abb Ag | Method for compensating disturbing influences in vibration type measuring instruments, involves transferring fluid medium in measuring pipe which is set into mechanical vibrations by excitation unit |
| DE102009012474A1 (en) | 2009-03-12 | 2010-09-16 | Endress + Hauser Flowtec Ag | Measuring system with a vibration-type transducer |
| DE102015122661A1 (en) | 2015-12-23 | 2017-06-29 | Endress + Hauser Flowtec Ag | Method for determining a physical parameter of a gas-laden liquid |
| DE102016109251A1 (en) * | 2016-05-19 | 2017-11-23 | Endress + Hauser Flowtec Ag | Vibration-type transducers |
| WO2019045703A1 (en) | 2017-08-30 | 2019-03-07 | Micro Motion, Inc. | Detecting and identifying a change in a vibratory meter |
-
2021
- 2021-07-22 DE DE102021118961.6A patent/DE102021118961A1/en active Pending
-
2022
- 2022-07-04 WO PCT/EP2022/068450 patent/WO2023001534A1/en active Application Filing
- 2022-07-04 CN CN202280050679.8A patent/CN117716214A/en active Pending
- 2022-07-04 EP EP22738662.0A patent/EP4374144A1/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| EP4374144A1 (en) | 2024-05-29 |
| DE102021118961A1 (en) | 2023-01-26 |
| WO2023001534A1 (en) | 2023-01-26 |
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